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Hypersonic Flow over a Blunt Body with Plasma Injection

Hypersonic Flow over a Blunt Body with Plasma Injection,10.2514/2.3835,Journal of Spacecraft and Rockets,J. S. Shang,J. Hayes,J. Menart

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Hypersonic Flow over a Blunt Body with Plasma Injection   (Citations: 6)
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Journal: Journal of Spacecraft and Rockets - J SPACECRAFT ROCKET , vol. 39, no. 3, pp. 367-375, 2002
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    • ...Modification in the flow field in the presence of a forward facing jet or plasma has been reported by Shang et al [2]...

    V. Kulkarni, et al. Drag reduction by counterflow supersonic jet for a blunt cone in high ...

    • ...The comparison of the computed shock structures with the Schlieren at an injection pressure of 582 kPa is depicted in Fig. 8. It becomes clear that the computed shock structure using the equilibrium air plasma injection captures all essential features of the plasma jet interaction [19, 20]...
    • ...Analyzing all the computations, the retraction of shock wave system by the air plasma injection is mostly associated with a reduced mass flow rate by the elevated plasma temperature [19, 20]...

    J. S. Shang. Hypersonic Magneto-Aerodynamic Interaction

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